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Experimental study of flame characteristics of ethylene and its mixture with methane and hydrogen in supersonic combustor 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 86, 页码: 775-781
Authors:  Zhong FQ(仲峰泉);  Cheng LW(程柳维);  Gu HB(顾红斌);  Zhang XY(张新宇)
Favorite  |  View/Download:20/0  |  Submit date:2019/05/29
Supersonic combustor  Hydrocarbon  Mixture fuel  Flame structure  Ignition  
Development of Skeletal Kerosene Mechanisms and Application to Supersonic Combustion 期刊论文
ENERGY & FUELS, 2018, 页码: 10.1021/acs.energyfuels.8b03350
Authors:  Yao W(姚卫);  Wu K(吴坤);  Fan XJ(范学军)
Adobe PDF(1388Kb)  |  Favorite  |  View/Download:75/17  |  Submit date:2018/12/27
Combustion Condition  Combustor Efficiency  Improved Delayed Detached Eddy Simulations  Initial Temperatures  Laminar Flame Speed  Scramjet Combustors  Supersonic Combustion  Turbulence-chemistry Interactions  
Application of conjugate gradient method for estimation of the wall heat flux of a supersonic combustor 期刊论文
Authors:  Cheng LW;  Zhong FQ(仲峰泉);  Gu HB(顾洪斌);  Zhang XY(张新宇);  Zhong, FQ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
Adobe PDF(1788Kb)  |  Favorite  |  View/Download:113/39  |  Submit date:2016/09/14
Conjugate Gradient Method  Inverse Heat Conduction Problem  Supersonic Combustor  Wall Heat Flux  
Numerical study of combustion and convective heat transfer of a Mach 2.5 supersonic combustor 期刊论文
APPLIED THERMAL ENGINEERING, 2015, 卷号: 89, 页码: 883-896
Authors:  Wang X;  Zhong FQ(仲峰泉);  Gu HB(顾宏斌);  Zhang XY(张新宇);  Zhong, FQ (reprint author), 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
Adobe PDF(4711Kb)  |  Favorite  |  View/Download:89/43  |  Submit date:2016/01/08
Supersonic Combustor  Convective Heat Transfer  Numerical Study  Wall Heat Flux  
An analytical theory of heated duct flows in supersonic combustors 期刊论文
Theoretical & Applied Mechanics Letters, 2014, 期号: 3, 页码: 31-35
Authors:  Wu CX(吴晨曦);  Zhong FQ(仲峰泉);  Fan J(樊菁)
Adobe PDF(193Kb)  |  Favorite  |  View/Download:90/28  |  Submit date:2015/09/02
Duct Flow With Heating  Self-similar Solution  Thermal Choking  Supersonic Combustor  
A coupled heat transfer analysis with effects of thermal/catalytic cracking of kerosene for regenerative cooled supersonic combustor 会议论文
23rd International Congress of Theoretical and Applied Mechanics, 中国北京/Beijing, China, 2012-08-19
Authors:  Wang X(王曦);  Zhong FQ(仲峰泉);  Chen LH(陈立红);  Zhang XY(张新宇)
Adobe PDF(113Kb)  |  Favorite  |  View/Download:268/77  |  Submit date:2014/04/02
Kerosene  Combustor  Thermal  Regenerative  Coupled  Catalytic  Cracking  Analysis  Supersonic  Transfer  Cooled  Effects  Board  Solving  Extra  Through  Differ  Energy  Cooling  Model  
Catalytic Cracking and Heat Sink Capacity of Aviation Kerosene Under Supercritical Conditions 期刊论文
Journal of Propulsion and Power, 2009, 卷号: 25, 期号: 6, 页码: 1226-1232
Authors:  Fan XJ(范学军);  Zhong FQ(仲峰泉);  Yu G(俞刚);  Li JG(李建国);  Sun CJ;  Fan XJ
Adobe PDF(2295Kb)  |  Favorite  |  View/Download:721/172  |  Submit date:2009/08/03
Fueled Supersonic Combustor  Model Combustor  Injection  
Effects of entry conditions on cracked kerosene-fueled supersonic combustor performance 期刊论文
Combustion Science and Technology, 2007, 卷号: 179, 期号: 10, 页码: 2199-2217
Authors:  Fan XJ(范学军);  Yu G(俞刚);  Li JG(李建国);  Yue LJ(岳连捷);  Zhang XY(张新宇);  Sung CJ;  Fan, XJ (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100080, Peoples R China.
Adobe PDF(1524Kb)  |  Favorite  |  View/Download:650/156  |  Submit date:2009/08/03
Entry Conditions  Kerosene  Supersonic Combustion  Thermal Cracking  Model Combustor  Propulsion  Injection  
Combustion of kerosene in a supersonic stream 会议论文
38th Aerospace Sciences Meeting and Exhibit 2000, Reno, NV, United states, January 10, 2000 - January 13, 2000
Authors:  Li JG(李建国);  Yu G(俞刚);  Zhang XY(张新宇);  Huang QS
Adobe PDF(519Kb)  |  Favorite  |  View/Download:21/12  |  Submit date:2017/06/01
Cavity Flame Holders  Combustion Efficiencies  Combustor Performance  Equivalence Ratios  Modular Structures  Optimized Conditions  Stagnation Pressures  Supersonic Combustors